Hence , they that flow field calculation and dynamical computation of fluid - solid coupling dynamic characteristics are carried out to search flow law in the hydraulic turbine , optimize the design of scroll casing , guide vane , blade and draft tube , and they can apply useful to the monitoring and fault diagnosis system of hydroelectric set as well 因此,为探求水轮机内部的流动规律,优化水轮机设计,为水轮机的安全稳定性运行和机组的故障诊断提供帮助。对导叶内部的流动进行流场计算和流固耦合振动特性的动力计算就显得十分必要。
The transient cfd simulation including the spiral case , stay vane , guide vane , runner vane and draft tube at different operation points is studied fitly , then the result of the pressure distribution on runner blade is provided for the runner transient structural simulation by fluid - structure interaction ( fsi ) method 文中首先对高水头小负荷的涡带工况下混流式水轮机内流场进行非定常cfd计算,得到涡带工况下叶片表面不同时刻的水压力载荷,并利用流固耦合方法对转轮进行结构场瞬态特性计算,分析转轮叶片的动应力特性。
The dynamo runs at rull speed to drive main shaft , then the main shaft makes the emulsifying wings in emulsification grove rotate , which absorbs the liquid in its brand groove into ring groove through guide vanes on upper and lower sides of the groove . the vanes spins circularly at high speed with the main shatf as center , and the blade and emulsificaton groove cut and crush it continuously . after that . it gers squeezed by the vanes highspeed centrifugal rotation . at last , it finishes isotropt emulsification tratment within extremely short time after continuous circulating mixing 由电动机全速运转带动主轴,经主轴转动乳化框槽内之乳化翼片,使其将桶槽内之液体经框槽上、下两侧之导流叶片吸入环状框槽内,经以主轴为中心高速圆周旋转叶片;连续使乳化翼端刀面与乳化框间极小之间系高频率之强力切割剪断、粉碎,再借叶片高速离心旋转排挤,持续循环混合,以极短之时间即可完成均质乳化之处理。
To meet the needs for wider surge margin of the turbofan engine , a new model was developed to predict the characteristics of the fan / high pressure compressor and turbine in this thesis . several ways , including , variable inlet guide vanes of the fan , variable guide vanes of the high pressure compressor , the variable inlet area ratio of the mixer and the nozzle areas , were presented to enlarge the surge margin of the turbofan engine . meanwhile , a method of combined variable geometries for optimizing controls of inlet guide vanes of the fan , guide vanes and the first two stators of high pressure compressor , area ratio of mixer and noz zle areas was established 为了满足下一代作战飞机对推进系统的性能和稳定性要求,本文建立了压缩系统特性和涡轮特性的新模型,并分别采用改变涡扇发动机风扇进口导流叶片、压气机导流叶片和前两级静叶片、混合室进口处内、外涵面积比和尾喷管面积,研究了其对发动机性能和稳定性的影响,进而得出了涡扇发动机变几何扩稳的方法,为发动机变几何扩稳研究打下理论基础。
In this paper , at first the cfd simulation including the spiral case , stay vane , guide vane , runner vane and draft tube at different operation points is studied , then the result of the pressure distribution on runner blade is provided for the runner structural simulation by fluid - structure interaction ( fsi ) method 本文首先对混流式水轮机全流道内流场进行了多工况的cfd计算,得到不同工况下转轮叶片表面水压力载荷,并利用顺序流固耦合方法对转轮在各种工况下的应力特性进行计算。